N512NK

Part: NONE — FAULT MESSAGE (ZONE 700) · airframe 56,813 hrs · 26,334 cycles

L/G GEAR NO DOWN LOCKED BOTH LGCIU'S INDICATED NOSE GEAR NOT DOWN AND LOCKED-R/R NLG LOCKSTAY ASSY IAW AMM 32-21-17. LEAK AND OPS TEST C/W. NO FAULTS DETECTED

Part: NONE — NONE · airframe 56,714 hrs · 26,280 cycles

L2 DOOR DAMPER BOTTLE REQUIRES NITROGEN SERVICES-SERVICED L2 DOOR DAMPER BOTTLE IAW AMM 52-10-00. NO LEAK NOTED

Part: MEGAPHONE — DAMAGED (ZONE 900) · airframe 54,995 hrs · 25,559 cycles

FWD MEGA PHONE DAMAGED-R&R FWD MEGA PHONE IAW A/C DRAWING NUMBER A319-EMER EQUIP

Part: NONE — NONE · airframe 54,893 hrs · 25,515 cycles

WHILE PERFORMING WEEKLY FOUND L2 DOOR ASSIST ACCUMULATOR LOW ON NITROGEN-SERVICED L2 DOOR ASSIST ACCUMULATOR PER AMM 52-10-00LEAK CHECK GOOD

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 54,811 hrs · 24,582 cycles

DURING LH ENGINE OPS CHECK- LEAK CHECK ENGINE #1FAILED TO SHUT DOWN CAUSING ENGINE EXHAUST FIRE--

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 54,811 hrs · 24,582 cycles

DURING LH ENGINE OPS CHECK- LEAK CHECK ENGINE #1FAILED TO SHUT DOWN CAUSING ENGINE EXHAUST FIRE--

Part: SKIN — DENTED (RT WING SLAT) · airframe 53,744 hrs · 25,037 cycles

REF MWI 2541174-1 WHILE PERFORMING WEEKLY CHECK FOUND DENT ON IBD RH SLAT-REPAIRED DENT ON RH WING #1 SLAT IAW A319 SRM TASK 57-40-00-300-109. THIS IS A CAT C TEMP REPAIR. REINSP AT 1FC. SUBSEQUENT INSP AT 750FC OR 750FH OR 120DAYS. REQUIRES PERMANENT REPAIR WITHIN 5000 FC/10,000 FH OR 24 MONTHS FROM EMBODIMENT PER SRI 57-40-00-205-030. THIS CLEARS MWI 2541174-1

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 53,637 hrs · 24,985 cycles

PASSENGER/CREW DOOR 842 DOOR ASSIST BOTTLE REQUIRES SERVICE-SERVICED DOOR 842 ASSIST BOTTLE W/ NITROGEN IAW AMM 52-10-00-614-001-A

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 53,637 hrs · 24,985 cycles

PASSENGER/CREW DOOR 832 DOOR ASSIST BOTTLE REQUIRES SERVICED-SERVICED DOOR 832 ASSIST BOTTLE WITH NITROGEN IAW AMM 52-10-00-614-001-A

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 52,416 hrs · 24,475 cycles

DURING RON CHECK FOUND MEGAPHONE TO BE INOP-R&R FWD MEGAPHONE IAW SPIRIT AIRLINES DRAWING NUMBER NK319-132-EQ

Part: UNKNOWN — FUMES (CABIN) · airframe 52,240 hrs · 24,401 cycles

FUME EVENT ON APPROACH CREW WENT ON O2. -REF TSM 05-50-00-810-831A APU VERIFIED NO LEAKS. PRE-CONDITIONES A/C W/APU NO SMELL NOTED. ISOLATED PACK 1+2 NO SMELL NOTED, RAN ENGINES + ISOLATED BLEEDS, NO SMELL NOTED. ALL STEPS ACCOMPLISHED W/ GEROTRACER ON BOARD. REF AMM 21-61-00-49-00-00,71-00-00. A/C OK FOR SERVICE.

Part: A/C PACK — ODOR (NR 1) · airframe 52,815 hrs · 24,373 cycles

FUME EVENT ON APPROACH IN COCKPIT-C/W IDENTIFICATION OF CABIN ODOR INSP. FOUND PACK 1 RESPONSIBLE PER TSM 05-50-00-810-831A

Part: ECS — CONTAMINATED · airframe 51,931 hrs · 24,269 cycles

SOLVENT / CHEMICAL SMELL ON APROACH BELOW 3.000FT-REF LG PAGE # 2534334-02 DR CONTAMINATION OF THE ENVIONMENTAL CONTROL SYS.

Part: UNKNOWN — ODOR (CABIN) · airframe 51,922 hrs · 24,265 cycles

DURING FINAL APPROACH SWEET SOLVENT ODOR SMELL NOTICED IN PAX CABIN AND COCKPIT-TROUBLESHOT IAW TSM 05-50-00-810-831-A. AEROTRACER DETECTED NO ODORS. A/C OK FOR CONTINUED OPERATION.

Part: A/C PACK — ODOR (NR 2) · airframe 51,927 hrs · 24,267 cycles

STRONG SOLVENT/FUME BELOW 10,000FT MSL FUME WENT AWAY WHEN PACK 2 WAS TURNED OFF-TROUBLE HSOT IAW TSM 05-50-00-810-801-A DETERMIND ODOR COMING FROOM PACK 2 SEE LOG PAGE 2534333-02 FOR PACK DEACTIVATION

Part: UNKNOWN — ODOR (CABIN) · airframe 51,871 hrs · 24,245 cycles

F/A REPORTS FUME EVENT-NOTICED AT ROW 11 AFT AND INCREASED IN INTENSITY MOVING AFT - BURNING - EXHAUST -OIL LIKE SMELL.-F/A REPORTED CABIN ODER EVENT PER TSM 05-50-00-810-831-A INSPECTED BOTH ENG AND APU OPERATED BOTH PACK WITH ISOLATED BLEED SOURCES FOUND NO EVIDENCE OF ODER AC OK FOR CONTINUED SVC.

Part: ENGINE — SMOKE (NR 2) · airframe 51,510 hrs · 24,069 cycles

PULLING INTO GATE, SHUT DOWN ENGINE #2 AND HAS A MASSIVE AMOUNT OF SMOKE CAME FROM ENGINE #2 AFTER SHUTDOWN NO ECAM MESSAGES DISPLAYED-VISUALLY INSPECTED AND PERFORMED ENGINE RUN/SHUTDOWN PER AMM 71-00-00 NO DEFECTS NOTED

Part: UNKNOWN — ODOR (AFT CABIN) · airframe 50,989 hrs · 23,808 cycles

AFT FA SMELL BURNING PLASTIC DURING DESCENT -PERFORMED FIM TASK 05-50-00-810-831-A RAN APU, #1 AND #2 ENGINES WITH CREW, CYCLED PACKS AND BLEEDS. INSPECTED A/C AND COULD NOT DUPLICATE SMELL . A/C OK FOR CONTINUED SERVICE

Part: UNKNOWN — FUMES · airframe 49,898 hrs · 23,328 cycles

FUMES ON T/O AND LANDING RELATED TO PACK 1 ( PACKS WITH MOD 31283/MP P7125 (FWC H2-F1 STND) AND WITH MOD. 30626/MP K6443 (ENHANCED ECS) - AT OR BELOW FL 370 )--

Part: SEAL — LEAKING (NR 1 DE OILER) · airframe 49,533 hrs · 23,190 cycles

FUMES SMELL IN COCKPIT ON ARRIVAL, SELECTED PACK 1 OFF FUMES DISSAPATED-C/W TSM 05-50-00-810-831-A. C/W COS REPORTING SHEET. FOUND TYPE 2 POSSIBLE CAUSE. C/W TSM 71-00-00-810-801. LEAK CHECK ENG #1. FOUND DEOILER SEAL LEAKING. R&R DEOILER SEAL IAW AMM 72-60-31. PERFORM DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYS. IAW AMM 21-00-00. NO SMELL NOTED. A/C OK FOR SVC.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 49,434 hrs · 23,148 cycles

F LOCKED FLAP-PERFORMED TROUBLE SHOOTING PER TSM 27-51-00-810-819-A FOUND L/H APPU SYNCHRO ANGLES IN EXCESS OF 5.2 PERFORMED VISUAL INSP OF TRANSMISSION ASSEMBLY PER AMM 27-54-00-200-001-A NO DEFECTS NOTED FOUND L/H APPU INSPECTION WINDOW FILLED WITH DEBRIS R/R L/H APPU PER AMM 27-51-18 OPS CHECK GOOD SYNCRO ANGLES WITING LIMITS WTB RESET PER AMM 27-50-00

Part: CABIN PRESSURE — OVERPRESSURED · airframe 48,866 hrs · 22,913 cycles

CAB PR EXCESS CAB ALT-PER TSM 21-31-00-810-806-A. OPS TEST WERE PERFORMED IAW AMM 21-31-00-710-002-A OPS TEST OF PRESSURE CONTROL & MONITORING, AMM 21-31-00-710-003-A OPS TEST OF MAN MODE SELC & MAN MODE PRESS CONT & FUNC TEST OF MAN MODE CAB ALT/FLOW VALVE POS INDICATION, AMM 05-53-00-780-001-A01 PRESS TEST. ALL OPS TEST NORMAL.

Part: MEGAPHONE — DAMAGED (AFT CABIN) · airframe 40,370 hrs · 23,098 cycles

DURING BATTERY CHANGE OF AFT MEGAPHONE, FOUND HARDWARE MISSING ON CAP-R/R AFT MEGAPHONE IAW AMM 25-65-51 AND SPIRIT DRAWING 319-EMER EQUIP, OPS CHECK GOOD

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 48,092 hrs · 22,574 cycles

AFT MEGAPHONE INOP. REPLACED AFT MEGAPHONE IAW NK319-132-EQ.

Part: UNKNOWN — ODOR (CABIN) · airframe 45,782 hrs · 32,558 cycles

OIL ODOR REPORTED FROM ROW 25 THRU AFT GALLEY, FOLLWED BY ELEC GEN 2 FAULT 2 MIN LATER SMELL LATER DISSAPATED PACK ISOLATION HAD NO EFFECT. IAW TSM 05-50-00-810-831A RAN PACKS APU AND ENGINES NO ODORS NOTED FROM EITHER PACK AIRCRAFT OK FOR SERVICE

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 45,469 hrs · 21,437 cycles

L1 DOOR ASSIST LOW PRESSURE. SERVICED THE DOOR ASSIST BOTTLE IAW AMM 52-10-00. LEAK CHECKED GOOD.

Part: BOX BEAM — CRACKED (FRAME 43) · airframe 45,062 hrs · 24,278 cycles

FRAME 43, STRINGER 15R, A CRACKED FOUND DURING EO 5330-1412. REPAIRED THE BOX BEAM FLANGE.

Part: SCUFF PLATE — GOUGED (L1 DOOR) · airframe 45,082 hrs · 21,278 cycles

GOUGE ON L1 DOOR FWD UNDER SCUFF PLATE AREA. COMPLIED WITH EO 5321-1795, REV 00. REPAIRED THE DOOR SCUFF PLATE.

Part: SKIN — DAMAGED (RUDDER) · airframe 45,082 hrs · 21,278 cycles

RUDDER SHELL AT THE NR 2 HOIST POINT DAMAGED 1,350 SQMM. REPAIRED THE RUDDER SHELL.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 44,564 hrs · 21,062 cycles

DURING A WEEKLY CHECK OF MAIN CABIN, FOUND THAT L1 DOOR ASSIST BOTTLE IS BELOW PRESSURE. THE DOOR ASSIST BOTTLE IAW AMM 52-10-00-210-004.

Part: SEAL — LEAKING (DE OILER) · airframe 43,179 hrs · 20,453 cycles

FUME EVENT ON TAKEOFF ROLL ON SLIGHT OIL ODOR IN CABIN AND COCKPIT. COM PROCEDURE WAS COMPLETED AND PACK NR 2 SHUT OFF FOR REMAINDER OF FLIGHT. PERFORMED TSM 05-50-810-831-A (CORS), FOUND THE NR 1 ENGINE DE-OILER OVERBOARD VENT LEAKING OIL. R & R MATING RING & SEAL ASSY IAW AMM 72-60-31. AS FAULT CONFIRMATION RAN BOTH ENGINES WITH BOTH PACKS ON, NO FUMES NOTED OR OIL ODOR AT THIS TIME IAW AMM 71-00-00.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 42,500 hrs · 20,142 cycles

MEGAPHONE DOES NOT WORK. R&R MEGAPHONE FWD GALLEY PER MM DRAWING NK319-132-EQ. OPS CK OK.

Part: SEAL — LEAKING (NR 1 DEOILER) · airframe 39,877 hrs · 18,972 cycles

ODORIN CABIN AND COCKPIT DURING TAXI IN ON NR 1 ENGINE, COCKPIT CREW SMELLED EXHAUST FUMES, ASKED FA'S ABOUT ODORS. THEY ALL SAID THEY SMELLED ODORS OF MUSTY, DIRTY SOCKS. THE 2 AFT F/A'S THEN SAID THAT DURING CLIMBOUT, THERE WAS A MUSTY ODOR. DE-BRIEFED CAPTAIN AND FOUND NR 2 ENGINE TO BE MAIN SOURCE OF THE ODOR. DURING EXTERNAL WALKAROUND OF THE NR 2 ENGINE, FOUND EXCESSIVE OIL LEAKING FROM DE-OILER BREATHER TUBE. REMOVED AND REPLACED THE NR 2 DE-OILER SEAL ASSY IAW AMM 72-60-32 PB 401, LEAK AND OPS CHECKED GOOD. PERFORMED NR 2 ENGINE IDLE RUN, ISOLATED NR 1 AND 2 PACKS AND FOUND NO COCKPIT OR CABIN ODORS PRESENT IAW AMM 71-00-00.

Part: OXYGEN MASK — DAMAGED (COCKPIT) · airframe 39,163 hrs · 18,640 cycles

F/O O2 MASK BAND SNAPPED AND DOES INFLATE. R & R F/O O2 MASK IAW AMM 35-12-41. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: ATTACH FITTING — CHAFED (LT MLG DOOR) · airframe 37,611 hrs · 17,939 cycles

LEFT FWD MLG DOOR KEELBEAM HINGE FWD ATTACH FITTING HAS CHAFE MARK ON INSIDE OF AFT WEB OF FITTING. COMPLY WITH EO 5336-1529, INTERIM REPAIR TO LT MLG DOOR ATTACHMENT. SDR ITEM. EO 5336-1529, REV 00, DATED 16DEC15; INTERIM REPAIR TO LT DOOR ATTACHMENT HAS BEEN COMPLIED WITH NON-ROUTINE.

Part: EPSU — FAULTED (EMERGENCY LIGHTS) · airframe 34,626 hrs · 16,546 cycles

DURING EPSU TEST AFTER SLIDE INSTALLATION L1 POSITION POWER SUPPLY SHOWED FAULT. R & R THE POWER SUPPLY IAW AMM 33-51-38. OPS CHECKED NORMAL.

Part: ATTACH FITTING — DAMAGED (MASK STRAP) · airframe 30,826 hrs · 14,851 cycles

F/O OXYGEN MASK INTERNAL CLIPS THAT HOLDS ONE OF THE INFLATABLE HEAD STRAPS TO THE MASK IS MISSING. R & R F/O OXYGEN MASK IAW AMM 35-12-14, PB 401.

Part: KNOB — MALFUNCTIONED (MEGAPHONE) · airframe 30,803 hrs · 14,840 cycles

AFT MEGAPHONE MISSING VOLUME REGULATOR KNOB. R & R AFT MEGAPHONE IAW AMM 25-65-51-710-002A. OPS CHECK OK.

Part: OXYGEN MASK — UNWANTED DEPLOY (ROW 1 DF) · airframe 30,780 hrs · 14,832 cycles

OXYGEN MASK DEPLOYED AT ROW 1DF. PERFORMED OXYGEN DROP TEST IAW AMM. OP'S CHECKED GOOD.

Part: DOOR SEAL — OBSTRUCTED (R1 DOOR) · airframe 30,136 hrs · 14,563 cycles

F/A REPORTED SOUND OF A LEAK FROM THE R1 DOOR. INSPECTED R1 DOOR SEAL IAW AMM FOUND LOOSE INTERIOR RUBBING STRIP BLOCKING MAIN SEAL AND SECURED. PERFORMED OPS CHECKED GOOD IAW AMM.

Part: DIAPHRAGM — PUNCTURED (R1 DOOR BOTTLE) · airframe 29,806 hrs · 14,424 cycles

R1 DOOR ASSIST BOTTLE DIAPHRAM PUNCTURED. R & R R1 DOOR ASSIST BOTTLE DIAPHRAM IAW AMM.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 29,431 hrs · 14,279 cycles

F/O MASK HARNESS DOES NOT INFLATE AND LEAKS FROM THE DEFLATED HARNESS AREA. R & R FULL FACE MASK IAW AMM. OPS CHECKED GOOD.

Part: ACM — ODOR (RIGHT) · airframe 29,159 hrs · 14,156 cycles

AFTER DEPARTURE ACFT HAD A LOUD RUMBING SOUND, FOLLOWED BY A SMOKE ODOR. F/A ANNOUNCED SMOKE IN CABIN. IAW CFM 05-50-00-810-831-A. FOUND ACM AT FAULT. DEACTIVATED RT PACK, PERFORMED ENGINE RUN IAW AMM 71-00-00-710-043 AND RAN BLEED SYS. NO SMOKE OR ODOR NOTED IN CABIN.

Part: OXYGEN MASK — FAULTED (CABIN) · airframe 28,560 hrs · 13,879 cycles

PAX OXYGEN PSU ROW 15DEF FAILED DROP TEST. WORK ACCOMPLISHED AND CLEARED ON NR 722N00127. R & R PAX OXYGEN PSU CONTAINER ASSY AT ROW 15DEF IAW AMM 35-21-41-000-001A & 35-21-41-400-001A. OPS CHECK GOOD IAW AZMM 35-23-00-710-001A.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 28,374 hrs · 13,794 cycles

L2 DOOR LOW PRESSURE OR DOOR ASSIST BOTTLE. SERVICED L-2 DOOR ASSIST BOTTLE TO PROPER PRESSURE IAW ACFT MM.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 28,178 hrs · 13,703 cycles

L2 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED L2 DOOR ASSIST BOTTLE IAW ACFT MM.

Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 27,518 hrs · 13,379 cycles

MEGAPHONE VOLUME CONTROL KNOB MISSING AT AFT GALLEY AREA. R & R MEGAPHONE AT AFT GALLEY AREA IAW ACFT MM. OPS CHECKED NORMAL.

Part: BOTTLE — LOW PRESSURE (L2 DOOR) · airframe 26,411 hrs · 12,855 cycles

L2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED L2 DOOR ASSIST BOTTLE ACCUMULATOR IAW MM.

Part: WARNING LIGHT — FALSE ACTIVATION (ELAC 1) · airframe 25,804 hrs · 12,560 cycles

ELAC 1 PITCH FAULT. PERFORMED RT BLUE ELEVATOR-SERVO CONTROL SERVO VALVE OPS TEST OF SIDE STICK ASSY. GROUND SCEN EFCS 1+2 NO FAULTS DETECTED. SYS CHECKS AND FUNCTION NORMAL.

Part: CYLINDER — LOW PRESSURE (PAX DOOR ASSIST) · airframe 25,678 hrs · 12,495 cycles

L2 PAX DOOR LOW PRESSURE. SERVICED L2 PAX DOOR TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: CHECK VALVE — CORRODED (ZONE 100) · airframe 22,444 hrs · 10,876 cycles

LOWER FUSELAGE AVIONICS EQUIPMENT VENTILATION AIR INLET CHECK VALVE WITH CORROSION. REPLACED SKIN AIR INLET CHECK VALVE IAW AMM TASK 21-26-52-000-001-A AND AMM 21-26-52-400-001-A.

Part: STRAP — CRACKED (RT WING TE FLAP) · airframe 22,444 hrs · 10,876 cycles

RT WING OTBD FLAP UPPER SURFACE STRAP CRACKED BETWEN RIB 16 AND 17. REPLACED STRAP PN 5757427620100 IAW SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 22,444 hrs · 10,876 cycles

FWD CARGO COMPARTMENT FR 26, FR 27 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK IAW TASK 25-41-000-001-A, SUB TASK 25-54-41-020-050 H.A(7) AND TASK 25-54-41-400-001-A, SUB TASK 25-54-41-420-050 H,B(6).

Part: BEARING — CORRODED (NLG DOOR) · airframe 22,444 hrs · 10,876 cycles

NLG DOOR LINKAGE AT HALF CLAMP AREA, BEARING CORRODED. REPLACED NLG DOOR LINKAGE AT HALF CLAMPS AND BEARING IAW AMM 32-22-17-400-001-A PARA 4C AND AMM 32-22-17-000-001-A PARA 4A(13),(15).

Part: GIRT BAR — CORRODED (R1 DOOR) · airframe 22,444 hrs · 10,876 cycles

UPPER FUSELAGE PAX CABIN R1 DOOR FWD AND AFT GIRT BAR FITTING BLANKING PLATES WITH CORROSION. REPLACED GIRT BAR FITTING PN D5311253400000 IAW SRM 51-72-11.

Part: ANGLE — CRACKED (ZONE 100) · airframe 22,444 hrs · 10,876 cycles

LOWER FUSELAGE AT FRAME 34 LEVEL STR 30 LT FAIRING SUPPORT SRUCTURE ANGLE CRACKED. REPLACED ANGLE IAW SRM 51-72-11.

Part: STRAP — WORN (NR 2 NACELLE) · airframe 22,444 hrs · 10,876 cycles

NR 2 ENGINE, NOSE COWLING, CAPPING STRAP WITH WORN AT 11 O`CLOCK. THE CAPPING STRAP WAS REPAIRED IAW SRM VRS2792 NR 030 PROCEDURE.

Part: TUBE — SCRATCHED (LT MLG) · airframe 22,444 hrs · 10,876 cycles

LEFT MLG SLIDING TUBE INBD SECTION WITH WEAR MARK. THE SLIDING REWORK REQUIRES A MINOR REPAIR (TEMPORARY OR LIFE LIMITED REPAIR) IAW MFG GUIDELINES.

Part: SKIN — CORRODED (ZONE 400) · airframe 22,444 hrs · 10,876 cycles

DURING INSPECTION, FOUND CORROSION AT THE ENGINE NR 2 PYLON AFT FAIRING INBD SKIN PANEL. REPLACED SKIN PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 22,444 hrs · 10,876 cycles

DURING INSPECTION, FOUND CORROSION AT THE UPPER FUSELAGE, PAX CABIN, FLOOR PANEL 221FF FWD SECTION. THE PANEL WAS REPLACED WITH NEW ONE.

Part: FITTING — CORRODED (ZONE 600) · airframe 22,444 hrs · 10,876 cycles

LEFT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING'S WITH CORROSION. THE FITTING'S REWORK REQUIRES A MAJOR REPAIR.

Part: FITTING — CORRODED (ZONE 500) · airframe 22,444 hrs · 10,876 cycles

LT WING, INNER REAR SPAR BETWEEN RIB 2 AND RIB 3, MLG RETRACTION JACK ANCHORAGE FITTING BORE AND SPOTFACE WITH CORROSION. THE FITTING REWORK REQUIRES A MAJOR REPAIR IAW GUIDELINES.

Part: SUPPORT — BROKEN (ZONE 100) · airframe 22,444 hrs · 10,876 cycles

LOWER FUSELAGE, LT AVIONIC COMPARTMENT AT C16 WASTE DUCT CLAMP ATTACH WITH SUPPORT BROKEN. REPLACED SUPPORT IAW SRM 51-72-11, PARG 4 AND 6.

Part: STRAP — CORRODED (LT WING TE FLAP) · airframe 22,444 hrs · 10,876 cycles

LT WING OTBD FLAP UPPER SURFACE STRAP IS CRACKED BETWEEN RIBS 16 AND 17. REPLACED STRAP IAW SRM 51-72-11.

Part: ATTACH ANGLE — CORRODED (ZONE 800) · airframe 22,444 hrs · 10,876 cycles

AFT FUSELAGE ACCESSORY COMPARTMENT ACCESS DOOR 312AR BONDING LEAD ATTACHMENT ANGLE CORRODED. REPLACED ANGLE IAW SRM 51-72-11.

Part: CYLINDER — LOW PRESSURE (L2 DOOR ASSIST) · airframe 21,063 hrs · 10,187 cycles

L2 DOOR ASSIST DAMPER PRESSURE LOW. SERVICED L2 DOOR ASSIST DAMPER TO PROPER PRESSURE IAW AMM 52-10-00-614-001.

Part: DOOR SEAL — LEAKING (ZONE 800) · airframe 18,926 hrs · 9,141 cycles

LOUD WHISTLING NOISE FROM L1 DOOR IAW TSM 52-11-00-810-826 SECTION 4A.(2) AND TSM TASK 52-11-00-810-811, PERFORMED T/S PROCEDURE OF THE L1 DOOR SEAL IAW AMM TASK 52-10-00-220-006 VISUAL INSP OF DOOR SEAL. L1 DOOR SEAL FOUND IN SERVICEABLE CONDITION. PRESSURIZED ACFT AND PERFORMED LEAK TEST OF THE L1 DOOR IAW AMM TASK 05-53-00-780-001. FOUND LEAK AT TOP OF RT AND BOTTOM LT CORNERS OF THE L1 DOOR. ADJUSTED THE L1 DOOR TOP RT AND BOTTOM LT CORNER STOP SCREWS IAW AMM TASK 52-11-00-820-001 SECTION 4B.(11). PERFORMED A MANUAL PRESSURIZATION REF AMM 05-53-00-780-001, VERIFIED ALL INDICATIONS WERE NORMAL AND NO LEAKS OR SQUEALS WERE NOTICED AT THE L1 OR ANY OTHER DOOR IN CABIN.

Part: INDICATOR — INOPERATIVE (FUEL SYSTEM) · airframe 18,555 hrs · 8,846 cycles

RT ENGINE FUEL FLOW INOP AND FUEL USED INOP. AFTER TAKEOFF, LOST OVER HALF OF LT TIP TANK FUEL AND LT ENGINE FUEL FLOW WAS 7900 LBS. IN CLIMB, SEEMS EXCESSIVE, ALL LT FUEL TANKS DRAINING FASTER THAN RT. FOLLOWED TSM 73-31-00-810-802, PERFORMED ENGINE RUN ON NR 1 & NR 2 ENGINES IAW AMM 71-00-00-710-043, FUEL INDICATION PERFORMED NORMAL WITH GREEN FUEL FLOW INDICATION. AS PRECAUTION, INSPECTED ALL CONNECTIONS TO EEC AND FUEL FLOW TRANSMITTER, NO DEFECTS OR LEAKS NOTED ON BOTH ENGINES. SUMPED FUEL TANKS IAW AMM 12-32-28-281-001, PERFORMED POST ENGINE RUN, AFTER 5 MINUTES, NO FAILURES DETECTED.

Part: CABIN PRESSURE — MALFUNCTIONED · airframe 18,231 hrs · 8,817 cycles

ACFT WOULD NOT PRESSURIZE AFTER T/O. AIR RETURN. PACKS OFF T/O. FIRST PACK ON AT 9360 FLASHING ADV SIGN. PRESSURE PAGE SHOWED OUTFLOW VALVE CLOSED. CABIN CONTINUED TO CLIMB. TURN ON PACK 2 STILL NO HELP. STOPPED CLIMB, SWITCHED TO MANUAL. NO JOY. SWITCHED PACKS OFF AND ON AGAIN AND MANUAL WORKED. TRIED AUTO AGAIN AND STILL NO JOY. CONTROLLED CABIN IN MANUAL. RETURN TO DEPARTURE. CONFIGURED TO SPEED 185 KTS. PERFORMED OPS CHECK OF THE PRESSURE CONTROLLER MONITORING IAW AMM 21-31-00-710-002. NO FAULTS NOTED. PERFORMED LEAK CHECK IN AIR CONDITIONER BAY IAW AMM 21-52-00-200-010. NO LEAKS NOTED. VISUALLY VERIFIED OUTFLOW VALVE WAS CLOSING. PERFORMED PRESSURIZATION CHECK OF CABIN IAW AMM 05-53-00-970-052. PERFORMED GENERAL WALK AROUND FOR ANY VISUAL DAMAGE AND FOUND NONE. ACFT OK FOR CONTINUED SERVICE.

Part: FITTING — CORRODED (CARGO BAY) · airframe 17,119 hrs · 8,308 cycles

AFT CARGO PIT LT WEDGE FITTING AND CARGO DOOR SFT PROFILE CORRODED BEYOND LIMITS

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

FLOORBEAM STA Y 1292 AT FRAME 66 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

FLOORBEAM STA Y1292 AT FR68 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

FLOORBEAM STA Y1292 L Z BEAM AT FRAME 66 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STA Y254 BETWEEN FRAMES 67 AND 68 HAS CORROSION.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

LEFT SHEAR PLATE HAS CORROSION.

Part: COOLING FAN — CORRODED (E/E BAY) · airframe 17,119 hrs · 8,308 cycles

RT AFT AVIONICS COMPARTMENT CORROSION ON THE BOTTOM F/O SKIN AIR INLET VALVE.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y765 AT FR67,68,AND 69 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y1292 AT FR 67 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y765 AT FRAME 68 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y1292 AT FR66 HAS CORROSION

Part: FRAME — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STA Y254 AT FRAME 67 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y254 ATFR68 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y300 AT FRAME 68 HAS CORROSION.

Part: FLOORBEAM — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

STATION Y765 AT FRAME 66 HAS CORROSION.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

RIGHT SHEAR PLATE HAS CORROSION.

Part: SHEAR PLATE — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

SHEAR PLATE SUPPORT HAS CORROSION.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 17,119 hrs · 8,308 cycles

FLOOR SUPPORT AT STATION Y1292 AT FR68 HAS CORROSION.